GB2528760B - Sliding connection between the floor structure and the hull structure of an aircraft. - Google Patents

Sliding connection between the floor structure and the hull structure of an aircraft. Download PDF

Info

Publication number
GB2528760B
GB2528760B GB1509321.4A GB201509321A GB2528760B GB 2528760 B GB2528760 B GB 2528760B GB 201509321 A GB201509321 A GB 201509321A GB 2528760 B GB2528760 B GB 2528760B
Authority
GB
United Kingdom
Prior art keywords
aircraft
sliding connection
hull
floor
floor structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
GB1509321.4A
Other versions
GB201509321D0 (en
GB2528760A (en
Inventor
Dazet Francis
Antypas Jérôme
Bel Laurent
Delorme Philippe
Brisbart Raphaël
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of GB201509321D0 publication Critical patent/GB201509321D0/en
Publication of GB2528760A publication Critical patent/GB2528760A/en
Application granted granted Critical
Publication of GB2528760B publication Critical patent/GB2528760B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/062—Frames specially adapted to absorb crash loads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/18—Floors
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00—Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49623—Static structure, e.g., a building component

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
GB1509321.4A 2014-05-30 2015-05-29 Sliding connection between the floor structure and the hull structure of an aircraft. Active GB2528760B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1454912A FR3021624B1 (en) 2014-05-30 2014-05-30 SLIDING CONNECTION BETWEEN THE FLOOR STRUCTURE AND THE HULL STRUCTURE OF AN AIRCRAFT.

Publications (3)

Publication Number Publication Date
GB201509321D0 GB201509321D0 (en) 2015-07-15
GB2528760A GB2528760A (en) 2016-02-03
GB2528760B true GB2528760B (en) 2020-07-08

Family

ID=51383848

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1509321.4A Active GB2528760B (en) 2014-05-30 2015-05-29 Sliding connection between the floor structure and the hull structure of an aircraft.

Country Status (5)

Country Link
US (1) US9764816B2 (en)
CN (1) CN105129068B (en)
CA (1) CA2891977A1 (en)
FR (1) FR3021624B1 (en)
GB (1) GB2528760B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3021625B1 (en) * 2014-05-30 2017-12-22 Airbus Operations Sas FLEXIBLE CONNECTION BETWEEN THE FLOOR STRUCTURE AND THE HULL STRUCTURE OF AN AIRCRAFT.
US11459085B2 (en) * 2019-04-30 2022-10-04 Textron Innovations Inc. Energy attenuation stabilizers and methods

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170968A (en) * 1986-05-12 1992-12-15 Scandanavian Bellyloading Company Ab Arrangement for loading a cargo compartment, in particular that of an aircraft, with piece goods
GB2444645A (en) * 2006-12-08 2008-06-11 Boeing Co Energy absorbing structure for aircraft
US20110042513A1 (en) * 2008-02-15 2011-02-24 Airbus Operations (S.A.S) Energy-absorbing structural element made of a composite material and aircraft fuselage having said absorber
WO2011073315A1 (en) * 2009-12-18 2011-06-23 European Aeronautic Defence And Space Company Eads France Energy absorption structural element made of composite material

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2113692A (en) * 1936-05-28 1938-04-12 Boeing Aircraft Co Fuel tank for aircraft
AU4166072A (en) * 1972-03-01 1973-11-01 Jury & Spiers Pty Ltd Clamping member
US6065267A (en) * 1998-10-09 2000-05-23 Tomcat Global Corporation V-shaped stackable truss that is selectively braceable
FR2864940B1 (en) * 2004-01-09 2007-03-30 Airbus France FIXING RAIL FOR AIRCRAFT
FR2877916B1 (en) * 2004-11-15 2008-04-25 Airbus France Sas AIRCRAFT FUSELAGE STRUCTURE FRAME
DE102005045181A1 (en) * 2005-09-21 2007-04-05 Eads Deutschland Gmbh Floor structure for aircraft
FR2891239B1 (en) * 2005-09-28 2009-04-17 Airbus France Sas FLOOR PANEL AND INSTALLATION FOR FIXING BUILDING ELEMENTS COMPRISING SUCH PANELS
DE102006019123B4 (en) 2006-04-25 2012-08-02 Airbus Operations Gmbh Soil structure for a hull
DE102007028098B4 (en) * 2007-06-19 2014-09-25 Airbus Defence and Space GmbH Airplane with hull shell and floor structure
US7967251B2 (en) * 2008-03-18 2011-06-28 The Boeing Company Truss network for aircraft floor attachment
DE102009012424B4 (en) * 2009-03-10 2014-03-20 Telair International Gmbh Cargo hold floor for a cargo hold of an aircraft and method for assembling such
FR2946008B1 (en) * 2009-05-28 2012-12-28 Airbus France AIRCRAFT COMPRISING FLOOR SUPPORT TRAILERS
DE102010014638B4 (en) * 2010-04-12 2019-08-01 Airbus Defence and Space GmbH Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage
DE102010027859B4 (en) * 2010-04-16 2017-11-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strut device for a cell, cell and vehicle
FR2975372B1 (en) * 2011-05-19 2013-07-05 Airbus Operations Sas AIRCRAFT INCLUDING IMPROVED MEANS FOR SUPPORTING A FLOOR STRUCTURE
FR2992628B1 (en) * 2012-06-28 2015-03-20 Airbus Operations Sas PRIMARY FUSELAGE STRUCTURE FOR AIRCRAFT COMPRISING ANTICIPATED BREAKING SPACERS TO INCREASE ENERGY ABSORPTION IN CASE OF CRASH.
DE102013205275B3 (en) * 2013-03-26 2014-10-02 Airbus Operations Gmbh Aircraft fuselage structure
CN105492318B (en) * 2013-07-12 2017-08-08 里尔喷射机公司 Door for aircraft
DE102013215228B3 (en) * 2013-08-02 2014-12-24 Airbus Operations Gmbh Aircraft fuselage structure
US10625844B2 (en) * 2014-11-10 2020-04-21 The Boeing Company Fuselage with structural and non-structural stanchions

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170968A (en) * 1986-05-12 1992-12-15 Scandanavian Bellyloading Company Ab Arrangement for loading a cargo compartment, in particular that of an aircraft, with piece goods
GB2444645A (en) * 2006-12-08 2008-06-11 Boeing Co Energy absorbing structure for aircraft
US20110042513A1 (en) * 2008-02-15 2011-02-24 Airbus Operations (S.A.S) Energy-absorbing structural element made of a composite material and aircraft fuselage having said absorber
WO2011073315A1 (en) * 2009-12-18 2011-06-23 European Aeronautic Defence And Space Company Eads France Energy absorption structural element made of composite material

Also Published As

Publication number Publication date
FR3021624B1 (en) 2017-12-22
US20150344119A1 (en) 2015-12-03
CN105129068A (en) 2015-12-09
FR3021624A1 (en) 2015-12-04
GB201509321D0 (en) 2015-07-15
GB2528760A (en) 2016-02-03
CA2891977A1 (en) 2015-11-30
CN105129068B (en) 2020-03-20
US9764816B2 (en) 2017-09-19

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